Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-104-1548 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
Alternate Parts: 5900T30G02, 5900T30G02, 2840-01-104-1548, 01-104-1548, 2840011041548, 011041548
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 28, 1980 | 01-104-1548 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-104-1548
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5900T30G02 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 5900T30G02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-104-1548
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 2.615 INCHES MINIMUM AND 2.635 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J85-94; 43 NOZZLES MAKE UP 1 NOZZLE ASSEMBLY,TURBINE,GAS TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85 |